KR101468339B1 - Automobile having flying function of helicopter - Google Patents

Abstract

The present invention relating to a helicopter type flying automobile includes a frame; an engine unit including an engine installed in the frame; an engine output unit extending from the engine unit and transferring the rotational force generated from the engine to one side of the frame; a rotor input shaft unit which transports the rotational force of the engine to a rotor by engaging one side thereof with the engine output unit; a rotor unit which is detachably connected to the other side of the rotor input shaft unit and includes the rotor controlling the vertical movement of the frame; a rotor direction diversion support unit which is fixed on a roof of the frame and supports the rotor input shaft unit to tilt left and right, and back and forth; a tail wing input shaft unit of which one side engages with one side of the rotor input shaft unit to transfer the rotational force of the engine unit to a tail wing.

Description

{AUTOMOBILE HAVING FLYING FUNCTION OF HELICOPTER}

[0001] The present invention relates to a flying vehicle, which is capable of traveling by automobile in normal times, and can easily carry out vertical takeoff and landing by helicopter type equipped with a rotor and a rotor shaft which are easily separated in a flight mode, It is about a helicopter flying car.

In the modern society, the penetration rate of automobile, which is a representative of land transportation, is increasing rapidly. On the contrary, when the rate of road securing and the rate of increase are not keeping up with the automobile penetration rate, traffic accidents and wasted oil have.

This kind of land transportation environment is getting worse, travel time and transportation cost are rising. As a countermeasure to this, fast air transportation means has been proposed. However, air transportation means can be easily operated by airplane, helicopter, There is a problem that access time and high cost are required.

Nowadays, as the area of activity such as travel and business becomes wider, decades later, it requires private air transportation, and it requires cheap airplanes that can be popularized.

As a result, there is a demand for an air transportation system that is simple in operation and safe and fast when it is used as an automobile for on-ground transportation at normal times and is changed to a flight mode easily when necessary.

1. A flying car (Patent No. 10-2003-0083449) 2. Combined vehicle for vertical takeoff and landing flight (Patent No. 10-2009-0116573)

SUMMARY OF THE INVENTION The present invention has been made in order to solve the above-mentioned problems, and it is an object of the present invention to provide an air conditioner which can be used as a vehicle for land transportation, The present invention aims at providing a helicopter type airplane which can take off and land vertically, has a simplified simplified component configuration necessary for flight, and is a low cost entry type, allowing a user to quickly move to a desired place.

A helicopter flying vehicle according to the present invention includes: a body; An engine unit including an engine mounted on the vehicle body; An engine output shaft portion extending from the engine portion and transmitting rotational force generated from the engine to one side of the vehicle body; A rotor input shaft portion having one side engaged with the engine output shaft portion and transmitting rotational force of the engine to the rotor; A rotor part detachably connected to the other side of the rotor input shaft part and including a rotor for controlling up and down of the vehicle body; A rotor direction switching support portion fixed to a roof of the vehicle body and supporting the rotor input shaft portion in such a manner as to be inclined forward, backward and leftward; A tail blade input shaft part having one side engaged with one side of the rotor input shaft part and transmitting rotational force of the engine part to a tail blade; A tail which adjusts the stop of the vehicle body and the switching of the vehicle body in the left and right direction to generate wind in a direction opposite to the direction in which the vehicle body is rotated so as to prevent the vehicle body from rotating in a direction in which the rotor is about to rotate, Wing portion; And a control link portion which is connected to the engine output shaft portion on one side and is connected to the control portion of the operator on the other side, and controls the engine output shaft portion in the forward, backward, left and right direction according to manipulation of the operator.

The engine output shaft portion includes a first engine output shaft having one side connected to an output shaft of the engine portion; An engine output shaft universal joint connected to the other side of the first engine output shaft; A second engine output shaft connected to the engine output shaft universal joint, the first engine output shaft being meshed with the first engine output shaft and coupled to be longitudinally reciprocable; And an engine output shaft portion bevel gear connected to the second engine output shaft and transmitting rotational force of the engine to one side of the vehicle body.

The rotor input shaft portion is engaged with the bevel gear of the engine output shaft portion, and receives a rotational force of the engine from the engine output shaft portion. A rotor input shaft universal joint connected to the rotor bevel gear; A first rotor shaft having one side detachably connected to the rotor input shaft universal joint; A second rotor shaft having the first rotor shaft coupled to one side and coupled to be longitudinally reciprocable; And a rotor shaft casing surrounding the rotor input shaft universal joint, the first rotor shaft, and the second rotor shaft.

The rotor unit 500 includes a plurality of rotors that are detachably connected to the other side of the second rotor shaft and generate a lifting force and a lowering force of the vehicle body.

      In addition, the rotor portion is connected to the edge portions of the rotors at one side and the rotor oil pressure regulating portion at the other side, and a plurality of rotor links for controlling the blade angle of the rotor by the operation of the rotor angle- .

Further, the rotor direction change support portion may include a rotor rotation bearing in which the rotor input shaft portion is inserted and supported; A pair of right and left switching shafts connected to the rotor rotating bearings in forward and backward directions and supported so as to be rotatable so as to face the rotor rotating bearings in the left and right direction; A first orbit part connected to the left and right changeover axes; A pair of front and rear switching shafts connected to the first orbiting portion in the left-right direction and supported in a left-right direction so as to be rotatable so that the first orbit portion and the rotor rotating bearing are directed in the front-rear direction; And a second orbit part connected to the forward / backward switching axis.

The tail wing input shaft portion may be a tail wing bevel gear which is engaged with the rotor bevel gear and receives the rotational force of the engine from the engine output shaft portion. A tail wing input shaft universal joint connected to the tail wing bevel gear; A first tail blade input shaft having one side connected to the tail blade input universal joint; And a second tail wing input shaft coupled to the first tail wing input shaft so as to be meshed with the first and second tail wing input shafts so as to be longitudinally reciprocable.

The tail wing portion is coupled to the other end of the second tail wing input shaft and receives a rotational force of the engine to convert the direction of the virtual rotation shaft from left to right in forward and backward directions. And a tail blade which is engaged with the tail blade connecting shaft to generate wind in a direction opposite to a direction in which the vehicle body is rotated to stop the vehicle body and to control the turning of the vehicle body in the left and right direction.

The control link unit may include: a sleeve for rotatably supporting the second engine output shaft; A first link rod having one side connected to the sleeve such that the sleeve and the second engine output shaft are movable in the front, rear, left, and right directions; A second link rod having one side connected to the other side of the first link rod; And a third link rod connected to the other side of the second link rod and connected to the steering wheel based on a hinge part provided on the lower side.

The helicopter type flying vehicle according to the present invention travels in a mode of driving the car at normal times and does not go to a separate airport. Instead, it loads and equips a rotor and a rotor shaft necessary for the flight at a desired time and place, It is possible to fly vertically by taking off and landing in a simple and stable way back and forth / right / left / up and down by the rotor direction change support part and rotor link in the stop state, and it is composed of at least simple parts which are reliable and necessary for flight, There is an effect that can provide air transportation.

1 is a perspective view of a helicopter flying vehicle according to the present invention;
2 is a perspective view of a rotor direction change support according to the present invention;
FIG. 3 is an operational view of the helicopter flying vehicle according to the present invention.
Fig. 4 is an operational view of the helicopter flying vehicle according to the present invention when it is reversed. Fig.
FIG. 5 is an operational view of a helicopter flying vehicle according to the present invention.
FIG. 6 is a view showing the operating state of the helicopter flying vehicle according to the present invention.
7 is a perspective view of a rotor portion according to the present invention.
8 is a conceptual view showing an application example of a rotor part according to the present invention.
9 is a perspective view showing a steering link portion according to the present invention.
FIG. 10 is an exploded view of a helicopter flying vehicle according to the present invention; FIG.

Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings.

FIG. 1 is a perspective view of a helicopter flying vehicle according to the present invention, FIG. 2 is a perspective view of a rotor direction switching support part according to the present invention, FIG. 3 is an operational state view of a helicopter flying vehicle according to the present invention, 4 is a view showing the operation state of the helicopter type airplane according to the present invention when the helicopter type airplane according to the present invention is reversed, FIG. 7 is a perspective view of a rotor unit according to the present invention, FIG. 8 is a conceptual view showing an application example of a rotor unit according to the present invention, FIG. 9 is a perspective view showing a steering link unit according to the present invention, Is an operating state diagram showing a flight assisted wing of a helicopter flying vehicle according to the present invention.

As shown in FIGS. 1 to 8, the helicopter flying vehicle 1000 according to the present invention includes a vehicle body 100; An engine unit 200 including an engine mounted on the vehicle body 100; An engine output shaft portion 300 extending from the engine portion 200 and transmitting rotational force generated from the engine to one side of the vehicle body; A rotor input shaft portion 400 having one side engaged with the engine output shaft portion 300 to transmit the rotational force of the engine to the rotor 520; A rotor part 500 detachably connected to the other side of the rotor input shaft part 400 and including a rotor 520 for controlling up and down of the vehicle body; A rotor direction switching support part 600 fixed to the roof 110 of the vehicle body 100 and supporting the rotor input shaft part 400 so as to be inclined in the front, rear, left and right directions; A tail blade input shaft part 800 having one side engaged with one side of the rotor input shaft part 400 to transmit the rotational force of the engine part 200 to the tail blade 820; A wind is generated in a direction opposite to the direction in which the vehicle body 100 is rotated so as to prevent the vehicle body 100 from rotating in a direction in which the rotor 520 is about to be rotated by engaging with the other side of the tail blade input shaft portion 800, A tail wing portion 800 for controlling the stopping of the vehicle body 100 and the lateral shift of the vehicle body 100; And a control link portion (not shown) for controlling the engine output shaft portion 300 in the forward, backward, leftward, or rightward direction according to an operation of the operator's control room 950, the other side being connected to the engine output shaft portion 300, 900).

The vehicle body 100 is a general passenger car including a seat, an engine, a frame, and a driving system in which a passenger can sit. In the present embodiment, a general passenger car is shown as a five-seater passenger car. However, .

The engine unit 200 is equipped with a piston of a passenger car and a cylinder type engine (not shown), includes a transmission (not shown), and can be mounted with an aviation engine such as another gas turbine engine.

3, the engine output shaft portion 300 includes a first engine output shaft 310 having one side connected to an output shaft of the engine portion; An engine output shaft universal joint 330 connected to the other side of the first engine output shaft 310; A second engine output shaft (320) connected to the engine output shaft universal joint (330), the first engine output shaft (310) meshingly inserted into the first engine output shaft (310) so as to be longitudinally reciprocable; And an engine output shaft bevel gear 340 connected to the second engine output shaft 320 to transmit the rotational force of the engine to one side of the vehicle body 100.

That is, the second engine output shaft 320 moves in the longitudinal direction to the left or right side in the drawing of FIG. 3 with respect to the first engine output shaft 310 by the sleeve 910 of the steering link unit 900, The total axial length of the engine output shaft 310 and the second engine output shaft 320 is increased and the length of the first engine output shaft 310 and the second engine output shaft 320 are reduced. Is engaged with the inner surface of the second engine output shaft 320 and is meshed with the gear type so that the rotational force is transmitted.

The engine output shaft universal joint 330 and the first engine output shaft universal joint 250 are general universal joints and function to transmit a rotational force even when the angle between the input shaft and the output shaft is changed.

The rotor input shaft portion 400 includes a rotor bevel gear 410 coupled to the engine output shaft portion bevel gear 340 in a vertical direction to receive the rotational force of the engine from the engine output shaft portion 300; A rotor input shaft universal joint 420 connected to the rotor bevel gear 410; A first rotor shaft 430 having one side detachably connected to the rotor input shaft universal joint 420; A second rotor shaft 440 coupled to the other side of the first rotor shaft 430 and coupled to be longitudinally reciprocable; And a rotor shaft casing 450 surrounding the rotor input shaft universal joint 420, the first rotor shaft 430, and the second rotor shaft 440.

The rotor input shaft universal joint 420 is a general universal joint and is capable of transmitting a rotational force even when the inclination angle of the first rotor shaft 430 is changed and is built in the vehicle body 100, A support bearing 455 is provided in the rotor shaft casing 450 so as to support the rotor shaft 440.

The first rotor shaft 430 is configured to be detachable and mountable from the rotor input shaft universal joint 420 and the second rotor shaft 440 is configured to be detachable and mountable from the first rotor shaft 430, When the vehicle is in a traveling mode other than the flight mode, the rotor shaft casing 450 can be detached and stored in a separate place or in a trunk of the vehicle body.

The rotor shaft casing 450 serves to separate and secure the passenger so that the first rotor shaft 430 and the second rotor shaft 440 are not in direct contact with each other.

The rotor unit 500 includes a plurality of rotors 520 detachably connected to the other side of the second rotor shaft 440 and generating a lifting force and a downward force of the vehicle body.

The number of such rotors 520 may be two, three, four or more.

In order to control the lifting force and the lowering force of the vehicle body, one side is preferably connected to the edge of each rotor 520 and the other side is connected to a rotor angle oil pressure regulator (not shown) A separate rotation shaft (not shown) is provided inside the rotor 520 at a boundary line portion where the second rotor shaft 440 is engaged by the operation of the hydraulic pressure regulating portion so that the rotor 520 can be rotated, And a plurality of rotor links 540 for adjusting the angle of attack.

The rotor 520 is fixed in such a manner that another fixing means formed at one end of the rotor 520 is inserted and fixed in the second rotor shaft 440, (530).

One end of the rotor link 540 is coupled to the outer side of the rotor 520 on the section thereof and the other end thereof is connected to the rotor oil pressure regulating part to pull the rotor 520 by the rotor oil pressure regulating part, By increasing the lift angle to increase the lift angle, the lift force can be increased or the rotor 520 can be pushed out to reduce the blade angle of attack of the rotor 520, thereby making it possible to increase the strength and control the altitude.

The rotor link 540 can be selectively omitted in the present embodiment. In this case, the rotor link 540 can be raised and lowered by adjusting the number of rotations of the rotor 520. The rotor link 540, The control unit utilizes a component configuration of a generally known helicopter, and can use a rotor link related component of a model helicopter or a general helicopter as shown in FIG. 8, and a detailed description thereof will be omitted.

As shown in FIG. 2, the rotor direction switching support part 600 includes a rotor rotation bearing 610 to which the rotor input shaft part 400 is inserted and supported; A pair of left and right switching shafts 620 connected to the rotor rotating bearings 610 in the front-rear direction and rotatably supported in the front-rear direction so that the rotor rotating bearings 610 are oriented in the left-right direction; A first orbit portion 630 connected to the left / right switching shaft 620; A pair of front and rear switching shafts 640 and 640 which are connected to the first orbit portion 630 in the right and left direction and which are supported in the left and right direction so as to be rotatable so that the first orbit portion 630 and the rotor rotation / ); And a second orbit portion 650 connected to the front / rear switching shaft 640 and fixed to the roof of the vehicle body 100.

5 and 6, when the manipulator 960 of the manipulator is operated in the left-right direction while the second rotor shaft 440 is inserted and supported in the rotor rotation bearing 610, The second engine output shaft 320 and the engine output shaft bevel gear 340 are moved in the left and right direction by the first and second rotor shafts 900 and 900. The rotor bevel gear 410 connected to the engine output shaft bevel gear 340, The second rotor shaft 440 which is viewed from the front is inclined with respect to the rotor direction change support portion 600. The rotor rotation bearing 610 is rotated while being rotated by the right and left change shaft 620, So that only the inclination of the shaft is changed while maintaining the position.

3 and 4, when the manipulator 960 is manipulated in the forward and backward direction, the second engine output shaft 320 and the engine output shaft bevel gear The rotor bevel gear 410 and the second rotor shaft 440 connected to the engine output shaft bevel gear 340 are moved in the front and rear direction and the second rotor shaft 440 viewed from the side is moved in the front- The first orbit portion 630, the left / right switching shaft 620, and the rotor rotation bearing 610 are rotated by the forward / backward switching shaft 640, And the slope of the shaft is changed while maintaining the position.

Accordingly, when the operator manipulates the rotor in the desired direction with the front, rear, left, and right freely, the rotor 520 finally connected to the second rotor shaft 440 tilts forward and backward and leftward to advance in the corresponding direction.

The tail wing input shaft portion 700 includes a tail wing bevel gear 710 coupled to the rotor bevel gear 410 and receiving the rotational force of the engine from the engine output shaft portion 300; A tail wing input shaft universal joint 720 connected to the tail wing bevel gear 710; A first tail wing input shaft 730 having one end connected to the tail wing input shaft universal joint 720; And a second tail wing input shaft 740, which is inserted into the first tail wing input shaft 730 by being meshed with the first tail wing input shaft 730 so as to be longitudinally reciprocable.

The tail wing input shaft universal joint 720 is a general universal joint and has a function of transmitting the rotational force even when the angle between the input shaft and the output shaft is changed.

That is, the first tail wing input shaft 730 moves in the longitudinal direction to the left or right in the drawing of FIG. 3, and the total axial length of the first tail wing input shaft 730 and the second tail wing input shaft 740 The outer surface of the second tail wing input shaft 740 is fitted to the inner surface of the first tail wing input shaft 730 so that the first gear wing input shaft 730 and the second tail wing input shaft 740 are engaged with each other. So that the rotational force is transmitted.

And a tail wing output shaft bevel gear 745 is provided on the other side of the second tail wing input shaft 740.

The tail wing portion 800 is engaged with the tail wing output shaft bevel gear 745 provided on the other side of the second tail wing input shaft 740 and the tail wing connection shaft input bevel gear 810a, A tail wing connecting shaft 810 for receiving the rotational force of the engine through the tail wing connecting shaft output bevel gear 810b and the tail wing input shaft 830 to switch the direction of the virtual rotational shaft from forward and backward directions to the left and right direction; And a tail wing 820 that adjusts the stop of the vehicle body 100 and the transverse direction of the vehicle body 100 by generating wind in a direction opposite to a direction in which the vehicle body 100 is rotated by engaging with the tail wing connecting shaft 810. [ ).

The wing angle of the tail wing 820 is controlled by a separate link portion (not shown) applied to a model helicopter or a general helicopter like the rotor portion 500 to generate wind by adjusting the blade angle of the tail wing 820 Direction can be adjusted.

The control link unit 900 includes a sleeve 910 for rotatably supporting the second engine output shaft 320, as shown in FIG. 9; A first link rod 920 having one side connected to the sleeve 910 such that the sleeve 910 and the second engine output shaft 320 are movable in the front, rear, left, and right directions; A second link rod 930 having one side connected to the other side of the first link rod 920; And a third link rod 950 connected to the other end of the second link rod 930 and connected to the steering wheel 960 on the basis of a hinge portion 940 provided on the lower side.

The hinge unit 940 is composed of a hinge fixture (not shown) and a hinge fixture (not shown) that partially surrounds the ball bearing and a ball bearing fixed to the vehicle body so that the third link rod 950 can move in the front, rear, do.

That is, when the control section 960 is moved forward, the third link rod 950, which is connected to the control section 960 with respect to the hinge section 940, moves backward and the second link rod 930 The first link rod 920, the sleeve 910, the second engine output shaft 320 and the engine output shaft bevel gear 340 move rearward and the rotor bevel gears 410, The second rotor shaft 440 and the rotor 520 are tilted forward by the rotor direction switching support portion 600 so that the vehicle body 100 is advanced.

Likewise, when the control section 960 is moved in a desired direction such as the left-right direction, the rotor 520 is operated in this way and finally the vehicle body 100 is tilted in the steering direction.

Meanwhile, the steering wheel 960 can be connected to and interlocked with the steering wheel of the driver in the driving mode of the vehicle. In the flying mode, when the steering wheel is moved in the front, rear, left, and right directions, the rotor 520 is operated When the handle is rotated in the clockwise or counterclockwise direction, the wind generation direction of the tail wing 820 is controlled to rotate the entire body 100. In addition, when the shift lever used in the vehicle running mode is raised and lowered And the angle of the wing angle of the rotor 520 is adjusted only when the button is pressed so that the up and down can be controlled. If the button is not pressed, the flight altitude can be maintained have.

On the other hand, as shown in FIG. 10, on both sides of the front and rear seats of the vehicle body 100, a first fly-assisting blade 150 or a second fly- And may further include an auxiliary blade 160. The flap may be mounted on the first or second flight assistant vane 150 or 160 so that the vehicle body 100 can be stably operated by interlocking with another drive system by a separate control unit Control.

As described above, the helicopter flying vehicle 1000 according to the present invention can control the tilting direction of the rotor 520 simply and accurately by the steering link portion 900 and the rotor direction change supporting portion 600, The first rotor shaft 430, the second rotor shaft 440, and the rotor portion 500 which are detached while the vehicle is normally traveling are combined and mounted, thereby being converted into a helicopter type air vehicle capable of vertical landing and landing by providing a simplified flight driving mechanism. It is possible to easily fly at a desired time and place, and thus it is possible to provide a low-priced popularized vehicle body.

While the present invention has been described in connection with what is presently considered to be practical exemplary embodiments, it is to be understood that the invention is not limited to the disclosed embodiments, but, on the contrary, Should be interpreted as falling within the scope of.

100: body 200: engine part
300: engine output shaft part 310: first engine output shaft
320: second engine output shaft 330: engine output shaft universal joint
340: engine output shaft bevel gear 400: rotor input shaft portion
410: Rotor bevel gear 420: Rotor input shaft universal joint
430: first rotor shaft 440: second rotor shaft
450: rotor shaft casing 500: rotor part
520: rotor 530: rotor cover
540: Rotor link 600: Rotor deflection support
610: Rotor rotation bearing 620: Left and right rotation axis
630: first orbital section 640:
650: second orbit portion 700: tail blade input shaft portion
710: Tail wing bevel gear 720: Tail wing input shaft universal joint
730: first tail wing input shaft 740: second tail wing input shaft
800: tail wing portion 810a: tail wing connecting axis input bevel gear
810b: Tail wing connection shaft output bevel gear 820: Tail wing
830: Tail blade input shaft 900: Steering link portion
910: Sleeve 920: First link rod
930: second link rod 940: hinge part
950: Third link load 1000: Helicopter flying car

Claims (9)

delete delete A body 100;
An engine unit 200 including an engine mounted on the vehicle body 100;
An engine output shaft portion 300 extending from the engine portion 200 and transmitting rotational force generated from the engine to one side of the vehicle body;
A rotor input shaft portion 400 having one side engaged with the engine output shaft portion 300 to transmit the rotational force of the engine to the rotor 520;
A rotor part 500 detachably connected to the other side of the rotor input shaft part 400 and including a rotor 520 for controlling up and down of the vehicle body;
A rotor direction switching support part 600 fixed to the roof 110 of the vehicle body 100 and supporting the rotor input shaft part 400 so as to be inclined in the front, rear, left and right directions;
A tail blade input shaft part 800 having one side engaged with one side of the rotor input shaft part 400 to transmit the rotational force of the engine part 200 to the tail blade 820;
A wind is generated in a direction opposite to the direction in which the vehicle body 100 is rotated so as to prevent the vehicle body 100 from rotating in a direction in which the rotor 520 is about to be rotated by engaging with the other side of the tail blade input shaft portion 800, A tail wing portion 800 for controlling the stopping of the vehicle body 100 and the lateral shift of the vehicle body 100; And
A control link portion 900 for controlling the engine output shaft portion 300 in the forward, backward, leftward, or rightward direction according to an operation of the operator's control portion 950, the other side being connected to the engine output shaft portion 300, ), ≪ / RTI >
The engine output shaft portion 300
A first engine output shaft (310) having one side connected to the output shaft of the engine section;
An engine output shaft universal joint 330 connected to the other side of the first engine output shaft 310;
A second engine output shaft (320) connected to the engine output shaft universal joint (330), the first engine output shaft (310) meshingly inserted into the first engine output shaft (310) so as to be longitudinally reciprocable; And
And an engine output shaft bevel gear 340 connected to the second engine output shaft 320 to transmit rotational force of the engine to one side of the vehicle body 100,
The rotor input shaft portion 400
A rotor bevel gear 410 coupled to the engine output shaft portion bevel gear 340 to receive the rotational force of the engine from the engine output shaft portion 300;
A rotor input shaft universal joint 420 connected to the rotor bevel gear 410;
A first rotor shaft 430 having one side detachably connected to the rotor input shaft universal joint 420;
A second rotor shaft 440 coupled to the other side of the first rotor shaft 430 and coupled to be longitudinally reciprocable; And
And a rotor shaft casing (450) surrounding the rotor input shaft universal joint (420), the first rotor shaft (430), and the second rotor shaft (440)
Helicopter flying car. The method of claim 3,
The rotor unit 500
And a plurality of rotors (520) detachably connected to the other side of the second rotor shaft (440) and generating a lifting force and a lowering force of the vehicle body
Helicopter flying car. 5. The method of claim 4,
And a plurality of rotors (520) for controlling the blade angle of rotation of the rotor (520) by the operation of the rotor angle oil pressure regulator by the operation of the controller, one side of which is connected to the edge of each rotor Further comprising a link 540
Helicopter flying car. A body 100;
An engine unit 200 including an engine mounted on the vehicle body 100;
An engine output shaft portion 300 extending from the engine portion 200 and transmitting rotational force generated from the engine to one side of the vehicle body;
A rotor input shaft portion 400 having one side engaged with the engine output shaft portion 300 to transmit the rotational force of the engine to the rotor 520;
A rotor part 500 detachably connected to the other side of the rotor input shaft part 400 and including a rotor 520 for controlling up and down of the vehicle body;
A rotor direction switching support part 600 fixed to the roof 110 of the vehicle body 100 and supporting the rotor input shaft part 400 so as to be inclined in the front, rear, left and right directions;
A tail blade input shaft part 800 having one side engaged with one side of the rotor input shaft part 400 to transmit the rotational force of the engine part 200 to the tail blade 820;
A wind is generated in a direction opposite to the direction in which the vehicle body 100 is rotated so as to prevent the vehicle body 100 from rotating in a direction in which the rotor 520 is about to be rotated by engaging with the other side of the tail blade input shaft portion 800, A tail wing portion 800 for controlling the stopping of the vehicle body 100 and the lateral shift of the vehicle body 100; And
A control link portion 900 for controlling the engine output shaft portion 300 in the forward, backward, leftward, or rightward direction according to an operation of the operator's control portion 950, the other side being connected to the engine output shaft portion 300, ), ≪ / RTI >
The rotor direction change support portion 600
A rotor rotation bearing 610 to which the rotor input shaft portion 400 is inserted and supported;
A pair of left and right switching shafts 620 connected to the rotor rotating bearings 610 in the front-rear direction and rotatably supported in the front-rear direction so that the rotor rotating bearings 610 are oriented in the left-right direction;
A first orbit portion 630 connected to the left / right switching shaft 620;
A pair of front and rear switching shafts 640 and 640 which are connected to the first orbit portion 630 in the right and left direction and which are supported in the left and right direction so as to be rotatable so that the first orbit portion 630 and the rotor rotation / ); And
And a second orbit portion 650 connected to the forward / backward switching shaft 640
Helicopter flying car. delete delete A body 100;
An engine unit 200 including an engine mounted on the vehicle body 100;
An engine output shaft portion 300 extending from the engine portion 200 and transmitting rotational force generated from the engine to one side of the vehicle body;
A rotor input shaft portion 400 having one side engaged with the engine output shaft portion 300 to transmit the rotational force of the engine to the rotor 520;
A rotor part 500 detachably connected to the other side of the rotor input shaft part 400 and including a rotor 520 for controlling up and down of the vehicle body;
A rotor direction switching support part 600 fixed to the roof 110 of the vehicle body 100 and supporting the rotor input shaft part 400 so as to be inclined in the front, rear, left and right directions;
A tail blade input shaft part 800 having one side engaged with one side of the rotor input shaft part 400 to transmit the rotational force of the engine part 200 to the tail blade 820;
A wind is generated in a direction opposite to the direction in which the vehicle body 100 is rotated so as to prevent the vehicle body 100 from rotating in a direction in which the rotor 520 is about to be rotated by engaging with the other side of the tail blade input shaft portion 800, A tail wing portion 800 for controlling the stopping of the vehicle body 100 and the lateral shift of the vehicle body 100; And
A control link portion 900 for controlling the engine output shaft portion 300 in the forward, backward, leftward, or rightward direction according to an operation of the operator's control portion 950, the other side being connected to the engine output shaft portion 300, ), ≪ / RTI >
The engine output shaft portion 300
A first engine output shaft (310) having one side connected to the output shaft of the engine section;
An engine output shaft universal joint 330 connected to the other side of the first engine output shaft 310;
A second engine output shaft (320) connected to the engine output shaft universal joint (330), the first engine output shaft (310) meshingly inserted into the first engine output shaft (310) so as to be longitudinally reciprocable; And
And an engine output shaft bevel gear 340 connected to the second engine output shaft 320 to transmit rotational force of the engine to one side of the vehicle body 100,
The manipulation link unit 900 includes:
A sleeve 910 for rotatably supporting the second engine output shaft 320;
A first link rod 920 having one side connected to the sleeve 910 such that the sleeve 910 and the second engine output shaft 320 are movable in the front, rear, left, and right directions;
A second link rod 930 having one side connected to the other side of the first link rod 920; And
And a third link rod 950 connected to the other side of the second link rod 930 and connected to the steering wheel 960 on the basis of a hinge portion 940 provided at the lower side
Helicopter flying car.

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